Experimental investigation of temperature and velocity distribution about a rocket jet
The purpose of the investigation was to determine the temperature distribution and velocity profile surrounding the wake of a 1500 pound thrust liquid rocket motor. The temperature measurements were restricted to those 500°F and below. The velocities measured were in the region in which the temperat...
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ndltd-CALTECH-oai-thesis.library.caltech.edu-49132019-12-22T03:08:54Z Experimental investigation of temperature and velocity distribution about a rocket jet Whitmore, Quentin Robert The purpose of the investigation was to determine the temperature distribution and velocity profile surrounding the wake of a 1500 pound thrust liquid rocket motor. The temperature measurements were restricted to those 500°F and below. The velocities measured were in the region in which the temperature measurements were made. The region in which the temperatures exceeded 500°F was found to be included within a solid angle of ten degrees. The high temperature region was found to be larger than the high velocity region. The investigation was carried out during the academic year 1946-1947 at GALCIT Jet Propulsion Laboratory under the supervision of Dr. Robert H. Boden. 1947 Thesis NonPeerReviewed application/pdf https://thesis.library.caltech.edu/4913/1/Whitmore_qr_1947.pdf https://resolver.caltech.edu/CaltechETD:etd-12092008-140117 Whitmore, Quentin Robert (1947) Experimental investigation of temperature and velocity distribution about a rocket jet. Engineer's thesis, California Institute of Technology. doi:10.7907/SN1E-KS25. https://resolver.caltech.edu/CaltechETD:etd-12092008-140117 <https://resolver.caltech.edu/CaltechETD:etd-12092008-140117> https://thesis.library.caltech.edu/4913/ |
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The purpose of the investigation was to determine the temperature distribution and velocity profile surrounding the wake of a 1500 pound thrust liquid rocket motor. The temperature measurements were restricted to those 500°F and below. The velocities measured were in the region in which the temperature measurements were made.
The region in which the temperatures exceeded 500°F was found to be included within a solid angle of ten degrees. The high temperature region was found to be larger than the high velocity region.
The investigation was carried out during the academic year 1946-1947 at GALCIT Jet Propulsion Laboratory under the supervision of Dr. Robert H. Boden.
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Whitmore, Quentin Robert |
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Whitmore, Quentin Robert Experimental investigation of temperature and velocity distribution about a rocket jet |
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Whitmore, Quentin Robert |
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Whitmore, Quentin Robert |
title |
Experimental investigation of temperature and velocity distribution about a rocket jet |
title_short |
Experimental investigation of temperature and velocity distribution about a rocket jet |
title_full |
Experimental investigation of temperature and velocity distribution about a rocket jet |
title_fullStr |
Experimental investigation of temperature and velocity distribution about a rocket jet |
title_full_unstemmed |
Experimental investigation of temperature and velocity distribution about a rocket jet |
title_sort |
experimental investigation of temperature and velocity distribution about a rocket jet |
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1947 |
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https://thesis.library.caltech.edu/4913/1/Whitmore_qr_1947.pdf Whitmore, Quentin Robert (1947) Experimental investigation of temperature and velocity distribution about a rocket jet. Engineer's thesis, California Institute of Technology. doi:10.7907/SN1E-KS25. https://resolver.caltech.edu/CaltechETD:etd-12092008-140117 <https://resolver.caltech.edu/CaltechETD:etd-12092008-140117> |
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AT whitmorequentinrobert experimentalinvestigationoftemperatureandvelocitydistributionaboutarocketjet |
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1719305154918875136 |